CN109641409A - Ribbon and its production method made of the prefabricated elements with substrate - Google Patents
Ribbon and its production method made of the prefabricated elements with substrate Download PDFInfo
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- CN109641409A CN109641409A CN201780047707.XA CN201780047707A CN109641409A CN 109641409 A CN109641409 A CN 109641409A CN 201780047707 A CN201780047707 A CN 201780047707A CN 109641409 A CN109641409 A CN 109641409A
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- rodpack
- ribbon
- pultrusion
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- 238000004519 manufacturing process Methods 0.000 title claims description 17
- 239000000758 substrate Substances 0.000 title claims description 15
- 239000011347 resin Substances 0.000 claims abstract description 23
- 229920005989 resin Polymers 0.000 claims abstract description 23
- 239000000835 fiber Substances 0.000 claims description 51
- 238000000034 method Methods 0.000 claims description 21
- 239000004744 fabric Substances 0.000 claims description 14
- 150000004767 nitrides Chemical class 0.000 claims description 5
- 239000011265 semifinished product Substances 0.000 description 14
- 238000005516 engineering process Methods 0.000 description 13
- 239000000463 material Substances 0.000 description 12
- 238000002347 injection Methods 0.000 description 10
- 239000007924 injection Substances 0.000 description 10
- 229920000049 Carbon (fiber) Polymers 0.000 description 3
- 238000005452 bending Methods 0.000 description 3
- 239000004917 carbon fiber Substances 0.000 description 3
- 238000001125 extrusion Methods 0.000 description 3
- 239000003365 glass fiber Substances 0.000 description 3
- 238000010030 laminating Methods 0.000 description 3
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 3
- 239000000203 mixture Substances 0.000 description 3
- 238000009966 trimming Methods 0.000 description 3
- 239000000284 extract Substances 0.000 description 2
- 238000001746 injection moulding Methods 0.000 description 2
- 238000009745 resin transfer moulding Methods 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000002950 deficient Effects 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 238000001035 drying Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 230000002344 fibroplastic effect Effects 0.000 description 1
- 238000009940 knitting Methods 0.000 description 1
- 238000003475 lamination Methods 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 239000012120 mounting media Substances 0.000 description 1
- 239000000047 product Substances 0.000 description 1
- 238000007711 solidification Methods 0.000 description 1
- 230000008023 solidification Effects 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
- 238000001721 transfer moulding Methods 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/68—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts by incorporating or moulding on preformed parts, e.g. inserts or layers, e.g. foam blocks
- B29C70/86—Incorporated in coherent impregnated reinforcing layers, e.g. by winding
- B29C70/865—Incorporated in coherent impregnated reinforcing layers, e.g. by winding completely encapsulated
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/02—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising combinations of reinforcements, e.g. non-specified reinforcements, fibrous reinforcing inserts and fillers, e.g. particulate fillers, incorporated in matrix material, forming one or more layers and with or without non-reinforced or non-filled layers
- B29C70/021—Combinations of fibrous reinforcement and non-fibrous material
- B29C70/023—Combinations of fibrous reinforcement and non-fibrous material with reinforcing inserts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/40—Shaping or impregnating by compression not applied
- B29C70/50—Shaping or impregnating by compression not applied for producing articles of indefinite length, e.g. prepregs, sheet moulding compounds [SMC] or cross moulding compounds [XMC]
- B29C70/52—Pultrusion, i.e. forming and compressing by continuously pulling through a die
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2031/00—Other particular articles
- B29L2031/08—Blades for rotors, stators, fans, turbines or the like, e.g. screw propellers
- B29L2031/082—Blades, e.g. for helicopters
- B29L2031/085—Wind turbine blades
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/70—Wind energy
- Y02E10/72—Wind turbines with rotation axis in wind direction
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
- Y02P70/00—Climate change mitigation technologies in the production process for final industrial or consumer products
- Y02P70/50—Manufacturing or production processes characterised by the final manufactured product
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Composite Materials (AREA)
- Mechanical Engineering (AREA)
- Moulding By Coating Moulds (AREA)
Abstract
The present invention relates to a kind of ribbon of the rotor blade of wind power plant (1), the ribbon is at least two pultrusion layers or RodPack layers (2a) (2b) (2c) and at least one tissue layer and/or basal layer (3a) (3b) (30a) (30b), the tissue layer and/or basal layer be arranged between at least two pultrusions layer or RodPack layers (2a) (2b) (2c) and/or the end of the tip side that is arranged in the pultrusion layer or RodPack layers (2a) (2b) (2c) in a manner of extending the pultrusion layer or RodPack layers (2a) (2b) (2c) on, wherein at least two pultrusions layer or RodPack layers (2a) (2b) (2c) and At least one described tissue layer and/or basal layer (3a) (3b) (30a) (30b) are connected with each other by resin mass.
Description
Technical field
The present invention relates to a kind of ribbons of the rotor blade of wind power plant and one kind for producing wind-power electricity generation
The method of the ribbon of the rotor blade of equipment.
Background technique
In general, there are two rotor blade half-shells for rotor blade tool.In rotor blade half-shell, substantially along maximum type
The line of material thickness is integrated with the ribbon made of fiber, so-called UD material, these fibers are arranged essentially parallel to rotor blade
Longitudinal axis extend, which has substantially intercepted bending load of the rotor blade on impact direction.In addition, usual edge
Rotor blade rear be integrated with the additional equally ribbon made of UD material, which has substantially intercepted rotor leaf
Piece bending load in a rotational direction.The main ribbon of the two rotor blade shells passes through at least one connecting element each other
It is connected.Rear ribbon is typically directly bonded to each other together.
Ribbon and interconnecting piece are arranged for giving rotor blade enough bending stiffnesses in operation.Such as from DE
It is known that manufacturing the band made of the stacked tissue layer arranged and/or basal layer with laminating technology in 10 2,008 055771 B4
Shape object.However, these ribbons must have relatively large cross section thus, to provide enough tensile strength in the longitudinal direction.
In addition, known such ribbon from 10 2,011 003560 B4 of DE, extends in the longitudinal direction wherein being laminated with
Rove.Its shortcoming is that the orientation by rove is very high to manufacture the cost of ribbon.
Summary of the invention
Therefore, the purpose of the present invention is to provide a kind of ribbon and a kind of method for manufacturing ribbon, the bands
Shape object has smaller cross section in the case where tensile strength is constant.
In terms of ribbon, which is realized by the ribbon of the feature with claim 1, preferred embodiment party
Formula is the theme of dependent claims.
Ribbon according to the present invention has at least two layers made of the material through pultrusion, especially two
RodPack layers and at least one tissue layer or basal layer, the tissue layer or basal layer be arranged at least two pultrusion at
The end of RodPack layers of tip side is arranged between type layer or RodPack layers and/or in a manner of extending RodPack layers,
Described at least two RodPack layers and at least one described tissue layer or basal layer be laminated.
RodPack layers are interpreted as the plane layer being made of the prefabricated elements that can be used to manufacture ribbon herein.Usually
Rove is laminated into pultrusion layer, rove be by fiber wire, especially glass fibre or carbon fiber or both mixture or
The beam that other fibers are constituted.These fibers are individually stored on roller, while being disengaged from roller and being supplied to layer as rove
Pressure technique.It is rove is laminated together and reach preferred identical outer shape in the laminating technology.The outside shape
Shape is rectangle preferably in the cross section being transversely to the machine direction in the current situation, however it can also be envisaged that other cross sections, especially go back
There is round, trapezoidal or square cross section.Cross section targetedly keeps identical in the longitudinal direction.The rove of lamination is referred to as
Bar.These bars are cut into preset length.Here, these bars have the width of about 7mm and the height of about 1-2mm, pultrusion
The indefinite length of layer；However it can also be envisaged that other sizes, especially it may also be assumed that the width of pultrusion layer be 8mm, 9mm,
10mm or any higher millimeter and height are 1mm, 2mm, 3mm, 4mm or any higher millimeter.By preset quantity
Bar be adhered on common mounting medium, preferably flowing material so that operate it is more convenient so that referred to as RodPack
Material substantially has the identical width of the ribbon to be produced with rotor blade.But ribbon according to the present invention
Conventional pultrusion layer can be used, these pultrusion layers have substantially rectangular cross-sectional configuration cross section and it is wide to making or
These pultrusion layers of person have width identical with ribbon to be produced or in these pultrusion layers placed side by side
Several modes obtain the width of ribbon, wherein it is preferred that need not more than four pultrusion layers placed side by side to obtain the phase
The strap width of prestige.
Based on its structure, i.e. the structure of the glass fibre or carbon fiber that extend in the longitudinal direction under final effect, pultrusion at
Type object or RodPack have high tensile strength in the longitudinal direction and have significantly lower transverse direction anti-along width and/or height
Tensile strength.Especially for the required stiffness and strength for reaching rotor blade structure, by multiple, at least two, preferably three, four
Or the pultrusion layer or RodPack of any higher amount are laminated and set arrangement, oriented sideways and assist it mutually in terms of length
It adjusts, to obtain ribbon thickness distribution corresponding with local buckling load.At the end of its root side and the end of its tip side
Portion, ribbon according to the present invention have its smallest thickness or cross-sectional area.Between two end, according to the present invention
Ribbon there is the range of maximum thickness or cross-sectional area.
Targetedly, pultrusion object or RodPack are provided as coiled material, can be incited somebody to action based on its small surface rigidity
RodPack is rolled.During producing rotor blade, pultrusion layer or RodPack material can be moved back from a roll of or multireel
It rolls up and is stacked up with being stacked.
Facts proved that big on profile depth direction in the region of the end of the root side of ribbon be laterally extended pair
RodPack material has an impact.Therefore, ribbon according to the present invention is knitted between two RodPack layers at least one
Nitride layer or basal layer, wherein the fiber in fabric or substrate is substantially oriented with 45 ° to 60 ° of positive and negative of positive and negative of angle.
In a kind of particularly advantageous characteristics of ribbon according to the present invention, fabric is placed between RodPack layers with 1: 4 ratio
The weight per unit area of layer or the fabric or basal layer of basal layer and drying in two primary fibre direction is about 800g/
m2。
Furthermore facts proved that, pultrusion layer or RodPack layers of desired width are wide to placing these layers can not
To until rotor blade be located next to, in the end of tip side because in the depth of this rotor blade or already less than drawing
Extrusion forming layer or RodPack layers of width and/or leading edge or rear are possibly into the region of main ribbon.According to this hair
Bright, pultrusion layer or RodPack layers terminate with the suitably distance of the distal end with rotor blade and according to the present invention by bases
Bottom is supplemented or is extended, these basal layers and pultrusion layer or RodPack stacking is set and the profile with rotor blade
Accordingly in the such trimming of its longitudinal direction side, so that these basal layers are adapted with the profile of rotor blade.
Draw together with all tissue layers or basal layer in all pultrusion layers that should form ribbon or RodPack layers
After entering in corresponding production mould, such as all layers are impregnated with resin mass by injection technology and thus make it in resin
Block is connected with each other during solidifying.
Facts proved that arranging one or more ± 45 ° of fabrics or ± 45 ° of substrate between RodPack layers individual
In the case where, the available most apparent raising of transverse tensile strength.± 45 ° of fabric refers to such fabric, two
Primary fibre direction is with longitudinal angular arrangement at+45 ° or -45 ° with RodPack layers.Also it has attempted to using ± 60 °
Substrate.However, highest transverse tensile strength is obtained when using about ± 45 ° of substrate, wherein even if use ± 45 ° ±
It is also yielded good result when 10 ° of substrate.
In another preferred embodiment of ribbon according to the present invention, in pultrusion layer or RodPack layers extremely
Few one is extended in tip side in the longitudinal direction by least one tissue layer or basal layer for having a primary fibre direction.
It is preferred that stacked arrange multiple tissue layers or basal layer, these tissue layers or basal layer to extend pultrusion in tip side
Layer or RodPack layers.Extend over pultrusion layer or RodPack layers of tissue layer or basal layer be trimmed and with pultrusion at
Type layer or RodPack layers are impregnated and are cured with resin with injection technology together.
The present invention is realized in its second aspect by the method for the feature with claim 7.
This method is particularly suitable for manufacturing one of above-mentioned ribbon.
Made above-mentioned ribbon is particularly in the rotor blade of wind power plant, these ribbons are especially main
Ribbon, these main ribbons are integrated on the longitudinal direction of rotor blade substantially along the highest structure height of rotor blade
In blade enclosure, these main ribbons substantially straight, are preferably completely formed as the crow flies in the longitudinal direction, and perpendicular to vertical
To, i.e. these ribbons can have the shape being adapted to the aerodynamic shape of rotor blade on profile depth direction.
According to the present invention, pultrusion layer or RodPack stacking are layered stacking with setting in the method, thus these pultrusions
Shape layer or RodPack layers are arranged so that its big area is stacked.Here, at least one times in pultrusion layer or RodPack layers
Root side end regions in arrange at least one tissue layer between two adjacent pultrusion layers or RodPack layers
And/or basal layer, and/or the end of pultrusion layer or RodPack layers of tip side with extend pultrusion layer or
RodPack layers of mode arranges at least one tissue layer and/or basal layer.By pultrusion object or RodPack and tissue layer and/
Or basal layer is mutually laminated together.
Used laminating technology is usually traditional injection technology, such as resin injection molding (resin injection
Moulding, RIM) technique or resin transfer molding (resin transfer moulding, RTM) technique, wherein will be preferably double
In the resin system injection semi-finished product of group fraction.During resin system solidified, the resin system generally go through exothermic peak and
Usually to the heat outside resin system supply after it have passed through exothermic peak, so that resin system generation is fully crosslinked simultaneously
So that laminate is fully cured.
It is also contemplated that for example select, based on using pre-impregnated tissue layer or basal layer (so-called preimpregnation
Material) production technology, wherein resin, which is present in uncured state, to be knitted in the case where resin is introduced into production mould
In nitride layer or basal layer.
It proposes in principle, individually produces ribbon in the method according to the invention, however it is also contemplated that will
Ribbon is placed on the semi-finished product of rotor blade half-shell as semi-finished product and then by rotor blade half-shell together with ribbon
It is laminated with injection technology.In the latter case, injection technology is used for rotor blade half-shell and ribbon simultaneously, and the
Injection technology is only used for ribbon and is individually used for rotor blade half-shell in a kind of situation, wherein then through prefabricated ribbon
It is integrated into before injecting blade enclosure in the structure construction of blade enclosure or is then bonded to each other two components.
At aspect according to the method for the present invention, additionally advantageously using band, there are two the tissue layers and/or base of primary fibre direction
Bottom, the two primary fibre directions with longitudinal direction at ± 45 ° to ± 90 ° of angle to orient；Advantageously, using ± 45 ° of fabric
Or substrate, these fabrics or substrate are arranged between adjacent pultrusion layer or RodPack layers.It is contemplated that by these
Tissue layer and basal layer individually or with any amount are embedded between pultrusion layer or RodPack layer, can by tissue layer with
Basal layer is embedded in two adjacent, three higher amounts and then self the follow or any drawing self followed
Between extrusion forming layer or RodPack layers.Therefore, pultrusion layer or the RodPack layers of ratio between tissue layer or basal layer
It assume that as any arbitrary proportion and change in the length of main ribbon.
According to the present invention it is possible to arrange between pultrusion layer or RodPack layers with the main fibre extended in the longitudinal direction
Tie up direction tissue layer or basal layer and its extend be more than pultrusion layer or RodPack layers of tip side end.It is passing through
Extended pultrusion layer or at least two of RodPack layers tip side end stretch out section between arrange above-mentioned knit
Nitride layer and/or basal layer are preferably as one-way fabric or substrate, and fiber is substantially arranged in these one-way fabrics or substrate
In longitudinal blade axis.
Detailed description of the invention
The present invention is described with five width figures by embodiment, in the accompanying drawings:
Fig. 1 a shows the sectional view of the ribbon according to the present invention with RodPack layers being transversely to the machine direction,
Fig. 1 b shows the sectional view of the ribbon according to the present invention with pultrusion layer being transversely to the machine direction,
Fig. 2 a shows the ribbon according to the present invention from Fig. 1 a in the region of RodPack layers of root side end
Perspective view,
Fig. 2 b shows the ribbon according to the present invention from Fig. 1 a or 1b in pultrusion layer or RodPack layers and general
Extended basal layer tip side end region in longitudinal section,
Fig. 3 is shown in which to arrange the vertical view of the end section of the rotor blade shell of with good grounds ribbon of the invention
Figure.
Specific embodiment
Fig. 1 a shows the sectional view of ribbon 1, and the ribbon band is there are three RodPack layers of 2a, 2b, 2c and is arranged in
Adjacent pultrusion layer or RodPack layers of two tissue layer or basal layer 3a, 3b between 2a, 2b, 2c.Quantity is only example
It lists to property, is usually provided with more RodPack layers, such as 20 to 40 RodPack layers of 2a, 2b, 2c.Tissue layer or substrate
Layer 3a, 3b can be set between all adjacent RodPack layer 2a, 2b, 2c or can also be provided only on several adjacent
RodPack layers between 2a, 2b, 2c.
RodPack layers of 2a, 2b, 2c refer respectively to it is multiple, in Fig. 1 be exactly four mutually side by side and in parallel with each other
Bar 4a, 4b, 4c, 4d of arrangement, the cross section of these bars be respectively configured to rectangle and herein preferably with 7mm width and
The height of 2mm.Bar 4a, 4b, 4c, 4d of RodPack layers of 2a, 2b, 2c are bonded on preferred associated carrier felt 5a, 5b, 5c.
Pultrusion layer 4a, 4b, 4c, 4d and carrier felt 5a, 5b, 5c collectively form RodPack layers of 2a, 2b, 2c.RodPack layers of 2a,
2b, 2c can be transversely to the machine direction L and be bent perpendicular to width B along height H, so that they can be to roll up on roller
Around mode transport.In order to manufacture ribbon 1, RodPack layers of 2a, 2b, 2c are cut into required length and along height
Degree H is stacked and sets.Arrange to have respectively in Fig. 1 between adjacent RodPack layer 2a, 2b, 2c tissue layer or basal layer 3a,
3b.RodPack layers of 2a, 2b, 2c natively have longitudinal L, which corresponds to longitudinal L of each bar 4a, 4b, 4c, 4d.
RodPack layers of 2a, 2b, 2c have big tensile strength in longitudinal directionl, but RodPack layers of 2a, 2b, 2c relative to
Cross force (being transversely to the machine direction the power that L pressed to or pulled RodPack layers of 2a, 2b, 2c along width B or height H) has small
Intensity.It is transversely to the machine direction L, RodPack layers of 2a, 2b, 2c only have smaller than RodPack layers of tensile strength in longitudinal directionl by about 10
To 30 times of tensile strength.
The reason of RodPack layers of 2a, 2b, 2c high tensile strength in longitudinal directionl is, bar 4a, 4b, 4c, 4d itself
Have in longitudinal directionl compared to along width B and the tensile strength considerably higher along the transverse tensile strength of height H, because
The fiber for essentially forming these bars equally orients in longitudinal directionl.Intensity of the bar on lateral B, H is only by the intensity of resinous substrates
In bar and thus it determines, because there is no fiber in RodPack in this direction.
Bar 4a, 4b, 4c, 4d used herein is manufactured with pultrude process, substantially that rove is laminated together herein.Slightly
Yarn can be for by the mixture of glass fibre or carbon fiber or both or there are also other fibroplastic beams, these beams while from simultaneously
It arranges and is disengaged on the roller arranged.Rove is laminated together using pultrude process and reaches cross section as bar 4a, 4b, 4c, 4d and is
Rectangle, shape with above-mentioned size, and it is then cut into required length.
For preferably operating stick 4a, 4b, 4c, 4d, by it along width B organized side-by-side and in a manner of organized side-by-side
It is bonded on carrier felt 5a, 5b, 5c.RodPack layer 2a, 2b, the 2c so generated can be rolled and more convenient as coiled material
It is transported and is handled in ground.
The cross section of the ribbon according to the present invention when being manufactured with pultrusion layer is illustrated in Fig. 1 b.Letter is drawn here
Example in, pultrusion plate have width identical with desired ribbon.But more elongated pultrusion also can be used
Profiled sheeting, it is then that its is placed side by side, with being preferably more than 4 blocks of plates placed side by side.In addition, being illustrated in the example of Fig. 1 a above
All the elements be also applied for the embodiment of the ribbon according to the present invention made of pultrusion layer.
The present invention one of in terms of it in be distinguished by: a is in the end of RodPack layers of root side according to fig. 2
Apply at least one tissue layer or basal layer 3a, 3b on RodPack layers of 2a, 2b, a 2c in region.RodPack layers of 2a,
The fiber of 2b, 2c have longitudinal L for determining of orientation by pultrusion layer, and tissue layer or basal layer 3a, 3b phase therewith herein
Anti- tool is there are two primary fibre direction H1, H2, the two primary fibre directions are by being interlaced with one another or the mutual direction shape of fiber that sutures
At.Primary fibre direction H1, H2 is interpreted as two such machine direction, i.e., the majority fibre of each tissue layer or basal layer 3a, 3b herein
Dimension is oriented along the two directions, but this does not change the feelings that fewer fiber can not extend along primary fibre direction
Condition.However, at least 30% however preferably at least 40% fiber each along each in the two primary fibre directions H1, H2
Person extends.Alternatively, two, three or more tissue layer can also be provided between 2a, 2b, 2c at two RodPack layers
3a, 3b, rather than tissue layer 3a, 3b.All embodiments in this chapter apply also for ribbon according to the present invention such as
Upper the case where being manufactured describedly by pultrusion plate.
The present invention one of in terms of it according to fig. 2 b in the tip side of pultrusion layer or RodPack layers of 2a, 2b, 2c
It is distinguished by the region of end, pultrusion layer or RodPack layers of 2a, 2b, 2c are in the tip side end of ribbon
Direction on by basal layer 3a, 3b, 3c extend；And it is, pultrusion layer or RodPack layers are in its corresponding tip side
Portion has inclined-plane, which ensures basal layer 3a, 3b, 3c from pultrusion layer or RodPack layers of 2a, 2b, 2c and cross its end
The smooth transition in portion.
The fiber that basal layer in the region of ribbon according to the present invention is distinguished by about 90% is fixed along it
To unique primary fibre direction H1, and specify on the direction B of ribbon lower than 10%, preferably shorter than 5% amount it is obvious
Lesser amount of transverse fiber, so that the fiber of unique primary fibre direction H1 gathers together and is basal layer 3a, 3b, 3c
Enough operational stabilities are provided.
In the embodiment in Fig. 1 a, 1b, 2a and 2b, a small amount of RodPack layers of 2a, 2b, 2c and a fabric are shown only
Layer or basal layer 3a, 3b, 3c.In ribbon according to the present invention, alternately band can also be provided on tissue layer 3a or 3c
There are other RodPack layers 2 of other tissue layers 3.The quantity of RodPack layers of 2a, 2b, 2c and tissue layer 3a, 3b can be more than 20
A layer, preferably greater than 30 layers, particularly preferably more than 40 layers.In principle, the quantity of RodPack layers of 2a, 2b, 2c are unrestricted
System, but be adapted with the demand for the rotor blade for being wherein equipped with ribbon 1.
In the embodiment of a according to fig. 2, there are two ± 45 ° of tissue layer 3c of primary fibre direction H1, H2 to be arranged for band
At make the two primary fibre directions H1, H2 be arranged to longitudinal direction angle L at 45 ° or -45° angle degree.The component is transferred to
On ribbon 1 with multiple RodPack layers of 2a, 2b, 2c and tissue layer 3a, 3b.It is however also envisaged that other angles position, especially
Itself it is also envisaged that, there are two primary fibre direction H1, H2, the two primary fibre directions are not relative to each other fabric itself tool
With angle in 90 °, but have for example into 120 ° of angle so that primary fibre direction H1, H2 can with longitudinal L
The mode of angle at 60 ° or the angle at -60 ° orients.
However, other relative angles between primary fibre direction H1, H2 of fabric are also also contemplated that, particularly preferably at 90 °
All relative angles within the scope of ± 10 °.
By tissue layer 3a, 3b, ribbon 1 is obtained compared to by direct layering stacked on top of each other, the drawing that contacts with each other
The transverse tensile strength that the ribbon 1 of extrusion forming layer or RodPack layers of 2a, 2b, 2c composition significantly improves.
Fig. 3 shows the end section of ribbon 1 in Fig. 1 in another aspect of the invention.End section should manage herein
Solution is the end of the tip side of ribbon.The top view of the tip side end of rotor blade shell can be seen in Fig. 3, completion
The profile 12 of outer profile 11 and UD layer 30a, 30b of the outer profile 10 of blade enclosure, pultrusion layer or RodPack layers of 2a, 2b
A part, the UD layers in tip pleurapophysis for pultrusion layer or RodPack layers of 2a, 2b.It is schematically illustrated in Fig. 3
Each 2 layers of pultrusion layer or RodPack layers of 2a, 2b, these layers prolong on the direction towards tip from UD layers of 30a, 30b respectively
It is long.But ribbon according to the present invention is not limited to 2 extended pultrusion layer or RodPack layers in distal direction,
But any number of pultrusion layers can be made in principle or RodPack layers extend in distal direction.
Pultrusion layer or RodPack layers of 2a, 2b, 2c are provided as coiled material and are cut by rotor blade length
Determining length.However it is difficult to, to pultrusion layer or RodPack layers of 2a, 2b, 2c trimming, namely make the change of its width
Carefully.
In the periphery of rotor blade, ribbon 1, which must attenuate, to be allowed it to protrude into outermost tip, and
And it must be designed more narrower than in the root area of rotor blade or in aerodynamics region.In order to enable ribbon 1
It reaches up in the outermost tip of rotor blade inner space, RodPack layers of 2a, 2b are cut into following length,
In these RodPack layers can also do not attenuate, i.e. trimming in the case where applied in inside in rotor blade inner space
It is added on rotor blade shell, and ribbon 1 passes through UD layers of 30a, 30b (unidirectional ply) from ribbon end on the direction of tip
It extends into tip.UD layers of 30a, 30b refer to tissue layer or basal layer with unique primary fibre direction L1.Principal fiber side
It is distinguished by L1, about 90%, preferably greater than 95% fiber extends along the direction.Primary fibre direction L1 is in longitudinal direction
It is oriented on L.
It proposing, UD layers of 30a, 30b extend to the end of the root side of ribbon 1 at RodPack layers between 2a, 2b,
It is contemplated that UD layers of 30a, 30b start in the end of the outermost root side of ribbon 1, extended RodPack layers of 2a,
The entire longitudinal extension of 2b and the end of the tip side of RodPack layers of 2a, 2b extend more than RodPack layers 2a, 2b.
By accessing UD layers of 30a, 30b between 2a, 2b at RodPack layers, ribbon 1 is more particularly at the end of the tip side of ribbon 1
Manufacture is very easy in portion region.
Ribbon 1 can individually produce.For this purpose, by above-mentioned pultrusion layer or RodPack layers of 2a, 2b, 2c and knitting first
Nitride layer or basal layer 3a, 3b, 30a, 30b are stacked or abreast layering is deposited in corresponding production mould.Then, it such as executes
Injection technology, wherein pultrusion layer or RodPack layers between 2a, 2b, 2c and tissue layer or basal layer 3a, 3b, 30a,
Resin system is injected in 30b and when necessary in the gap also between bar 4a, 4b, 4c, 4d of RodPack layers of 2a, 2b, 2c.
There is provided in principle it is two different for manufacture the methods for having the rotor blade half-shell of ribbon 1, wherein one
Ribbon 1 is individually produced in a variant first, such as by injection technology, and places the half of ribbon 1 in the second variant
The semi-finished product of finished product and rotor blade half-shell and then by the semi-finished product of rotor blade half-shell include ribbon 1 semi-finished product one
Injection technology is reinstated to be laminated.No matter which kind of variant is selected, and semi-finished product can be all put into process units.Then, by true
Empty film seals the semi-finished product for being layered stacking in process units stackedly on the inside of forming shell, that is, vacuum diaphragm is placed on semi-finished product
Above and by the vacuum diaphragm it is sealed on the edge of production half-shell.Then pass through input and outgoing line for preferred two pack system
Resin system injects in semi-finished product and extracts air out first, and then after with resin system pre-impregnated semi-finished product via leading
Pipeline extracts extra liquid resin system out from semi-finished product out.If semi-finished product are impregnated by resin completely, solidification process
It will be started in the form of heat-producing chemical reaction.After exothermic peak, usually supplied to resin system or impregnated semi-finished product
External heat is usually provided with thermophore in molding half-shell thus or outside is provided with heat radiator or thermophore.It is logical
Crossing external supply heat is fully cured resin system.
As a result it proves it is advantageous that ribbon 1 is produced independently of rotor blade half-shell, because thus, it is possible to EARLY RECOGNITIONs
It has the failure being likely to occur in ribbon 1 and does not then continue to manufacture rotor leaf using possible defective ribbon 1
Piece shell.
Ribbon 1 according to the present invention is by using pultrusion object or RodPack substantially straight landform in longitudinal directionl
At so that ribbon according to the present invention 1 especially in longitudinal directionl along rotor blade half-shell inner wall part extend and
The main ribbon being bonded at the inner wall part.In principle it is contemplated that this method is also used for rear ribbon, thus for example
Ribbon 1 may not be carried out in the whole length of rotor blade it is prefabricated, but may prefabricated rear ribbon straight area
Section and then piecewise is integrated in rotor blade half-shell.
List of numerals
1 ribbon
RodPack layers of 2a
RodPack layers of 2b
RodPack layers of 2c
3a tissue layer or basal layer
3b tissue layer or basal layer
3c tissue layer or basal layer
4a bar
4b bar
4c bar
4d bar
5A carrier felt
5b carrier felt
5c carrier felt
10 outer profiles
11 outer profiles
12 profiles
UD layers of 30a
UD layers of 30b
L is longitudinal
The primary fibre direction of L1 UD substrate
B width
H height
H1 primary fibre direction
H2 primary fibre direction
Claims (10)
1. a kind of ribbon (1) of rotor blade of wind power plant, the ribbon has at least two pultrusion layers
Or RodPack layers (2a) (2b) (2c) and at least one tissue layer and/or basal layer (3a) (3b) (30a) (30b), the fabric
Layer and/or basal layer are arranged between at least two pultrusions layer or RodPack layers (2a) (2b) (2c) and/or to prolong
The mode of the long pultrusion layer or RodPack layers (2a) (2b) (2c) are arranged in the pultrusion layer or RodPack layers
On the end of the tip side of (2a) (2b) (2c), wherein at least two pultrusions layer or RodPack layers (2a) (2b)
(2c) and at least one described tissue layer and/or basal layer (3a) (3b) (30a) (30b) pass through cured resin mass phase each other
Even.
2. ribbon (1) according to claim 1,
It is characterized in that, being provided between adjacent pultrusion layer or RodPack layers (2a) (2b) (2c) with following fine
Tie up direction tissue layer and/or basal layer (3a) (3b), the machine direction with (2a) RodPack layers described (2b) (2c)
Longitudinal (L) angled mode arranges.
3. according to claim 1 or 2 described in any item ribbons (1),
It is characterized in that, there are two primary fibre direction (H1) (H2), the two masters for the tissue layer or basal layer (3a) (3b) tool
Machine direction with longitudinal direction (L) at ± 45 ° to ± 90 ° of angle to orient.
4. ribbon (1) according to claim 3,
It is characterized in that, the primary fibre direction (H1) (H2) with longitudinal direction (L) at ± 45 ° of angle to orient.
5. according to the described in any item ribbons of the claims (1),
It is characterized in that, arranging have at least one on longitudinal direction (L) between at least two RodPack layers (2a) (2b) (2c)
A tissue layer or basal layer (30a) (30b) with primary fibre direction (L1) and described with primary fibre direction (L1) is knitted
It is more than at least two RodPack layers (2a) (2b) (2c) that nitride layer or basal layer, which extend on longitudinal direction (L) in tip side,.
6. ribbon (1) according to any one of claims 1 to 5,
It is characterized in that, being trimmed along its longitudinal direction side to rotor blade leading edge and rear through extended section.
7. a kind of method for producing ribbon,
It is layered wherein stackedly and stacks pultrusion layer or RodPack layers (2a) (2b) (2c), and is adjacent at least two
At least one basal layer and/or tissue layer (3a) (3b) are arranged between RodPack layers (2a) (2b) (2c), and/or described
The end of the tip side of RodPack layers (2a) (2b) (2c) is to extend the pultrusion layer or RodPack layers (2a) (2b)
The mode of (2c) arranges at least one tissue layer or basal layer 30a, 30b, and
Make the pultrusion layer or RodPack layers and basal layer and/or tissue layer 2a, 2b, 2c, (3a) (3b) (30a) (30b)
It is connected with each other by resin system.
8. according to the method described in claim 7,
It is characterized in that, there are two the tissue layer and/or basal layer (3a) (3b) tools primary fibre direction (H1) (H2), the two
Primary fibre direction with longitudinal direction (L) at ± 45 ° to ± 90 ° of angle to orient.
9. according to the method described in claim 8,
It is characterized in that, the primary fibre direction (H1) (H2) with longitudinal direction (L) at ± 45 ° of angle to orient.
10. method according to any one of claims 7 to 9,
It is characterized in that, by with the tissue layer of primary fibre direction (L1) and/or basal layer (30a) extended on the longitudinal axis (L),
(30b) is arranged between the pultrusion layer or RodPack layers (2a) (2b) (2c) and makes the tissue layer and/or substrate
Layer extends the end of the tip side more than the pultrusion layer or RodPack layers (2a) (2b) (2c).
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE102016009640.3A DE102016009640A1 (en) | 2016-08-10 | 2016-08-10 | Belt made of prefabricated elements with clutch and a method for its manufacture |
| DE102016009640.3 | 2016-08-10 | ||
| PCT/EP2017/070156 WO2018029240A1 (en) | 2016-08-10 | 2017-08-09 | Spar cap made of prefabricated elements with laid fabric and method for producing same |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN109641409A true CN109641409A (en) | 2019-04-16 |
| CN109641409B CN109641409B (en) | 2022-02-18 |
Family
ID=59581930
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201780047707.XA Active CN109641409B (en) | 2016-08-10 | 2017-08-09 | Strip made of prefabricated elements with a substrate and method for producing same |
Country Status (7)
| Country | Link |
|---|---|
| EP (1) | EP3496936B1 (en) |
| CN (1) | CN109641409B (en) |
| DE (1) | DE102016009640A1 (en) |
| DK (1) | DK3496936T3 (en) |
| ES (1) | ES2937720T3 (en) |
| PT (1) | PT3496936T (en) |
| WO (1) | WO2018029240A1 (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113272119A (en) * | 2018-11-28 | 2021-08-17 | 西门子加美萨可再生能源服务有限公司 | Rotor blade comprising a strip with deformable pultrusion |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102018006085A1 (en) * | 2018-08-02 | 2020-02-06 | Senvion Gmbh | Tapered pultrudate belt and a process for its manufacture |
| US10895244B2 (en) | 2018-09-25 | 2021-01-19 | General Electric Company | Joint interface for wind turbine rotor blade components |
| WO2020091783A1 (en) | 2018-11-01 | 2020-05-07 | General Electric Company | Scarf connection for a wind turbine rotor blade |
| DE102018009338A1 (en) | 2018-11-28 | 2020-05-28 | Senvion Gmbh | Rotor blade component, process for its manufacture and wind turbine |
| DE102019000052A1 (en) * | 2019-01-08 | 2020-07-09 | Senvion Gmbh | Rotor blade with at least one belt with a plurality of pultrudates and a method for its production |
| DK180532B1 (en) | 2019-04-23 | 2021-06-10 | Envision Energy Denmark Aps | A WIND WINDOW WING AND A METHOD FOR MANUFACTURING THE WIND WIND WING |
| US11131290B2 (en) | 2019-06-25 | 2021-09-28 | General Electric Company | Scarf connection for a wind turbine rotor blade |
| CN115485128A (en) * | 2020-04-28 | 2022-12-16 | Lm风力发电公司 | Optimized spar cap structure for wind turbine blades |
| EP4143014A1 (en) * | 2020-04-28 | 2023-03-08 | LM Wind Power A/S | Optimized interlayer for a spar cap for a wind turbine blade |
| EP4143013A1 (en) | 2020-04-28 | 2023-03-08 | LM Wind Power A/S | An interlayer, a spar cap and a wind turbine blade |
| EP4108439A1 (en) * | 2021-06-25 | 2022-12-28 | LM Wind Power A/S | Spar cap with tapering and serrated end section |
| CN113339188B (en) * | 2021-06-29 | 2024-04-09 | 三一重能股份有限公司 | Wind power blade main beam structure, preparation method thereof and wind power blade |
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- 2017-08-09 ES ES17751381T patent/ES2937720T3/en active Active
- 2017-08-09 PT PT177513819T patent/PT3496936T/en unknown
- 2017-08-09 DK DK17751381.9T patent/DK3496936T3/en active
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Also Published As
| Publication number | Publication date |
|---|---|
| EP3496936A1 (en) | 2019-06-19 |
| WO2018029240A1 (en) | 2018-02-15 |
| PT3496936T (en) | 2023-02-13 |
| DK3496936T3 (en) | 2023-01-23 |
| CN109641409B (en) | 2022-02-18 |
| DE102016009640A1 (en) | 2018-02-15 |
| EP3496936B1 (en) | 2022-11-30 |
| ES2937720T3 (en) | 2023-03-30 |
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Effective date of registration: 20220810 Address after: Hamburg, Germany Patentee after: Siemens COMESA renewable energy services Co.,Ltd. Address before: Hamburg, Germany Patentee before: SENVION SE |